CH413665A - Flexible folding tail for moving bodies, especially missiles - Google Patents

Flexible folding tail for moving bodies, especially missiles

Info

Publication number
CH413665A
CH413665A CH813163A CH813163A CH413665A CH 413665 A CH413665 A CH 413665A CH 813163 A CH813163 A CH 813163A CH 813163 A CH813163 A CH 813163A CH 413665 A CH413665 A CH 413665A
Authority
CH
Switzerland
Prior art keywords
moving bodies
flexible folding
folding tail
missiles
especially missiles
Prior art date
Application number
CH813163A
Other languages
German (de)
Inventor
Werner Dr Ing Habil Gohlke
Original Assignee
Gohlke Werner
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=7125167&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CH413665(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Gohlke Werner filed Critical Gohlke Werner
Publication of CH413665A publication Critical patent/CH413665A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16—Wrap-around fins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • B64C9/36—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
CH813163A 1962-07-11 1963-07-01 Flexible folding tail for moving bodies, especially missiles CH413665A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEG35435A DE1159314B (en) 1962-07-11 1962-07-11 Elastic folding tail, especially for flying bodies

Publications (1)

Publication Number Publication Date
CH413665A true CH413665A (en) 1966-05-15

Family

ID=7125167

Family Applications (1)

Application Number Title Priority Date Filing Date
CH813163A CH413665A (en) 1962-07-11 1963-07-01 Flexible folding tail for moving bodies, especially missiles

Country Status (3)

Country Link
US (1) US3165281A (en)
CH (1) CH413665A (en)
DE (1) DE1159314B (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1199664B (en) 1962-09-11 1965-08-26 Dynamit Nobel Ag Folding tail, especially for rocket projectiles
DE1428717C2 (en) * 1964-09-28 1974-05-30 Dynamit Nobel Ag Tail fairing for rockets with central nozzle and folding tail
US3304030A (en) * 1965-09-24 1967-02-14 James E Weimholt Pyrotechnic-actuated folding fin assembly
SE339646B (en) * 1970-01-08 1971-10-11 Bofors Ab
US3826448A (en) * 1972-09-14 1974-07-30 Nasa Deployable flexible ventral fins for use as an emergency spin-recovery device in aircraft
US3964391A (en) * 1973-09-04 1976-06-22 The United States Of America As Represented By The Secretary Of The Army Dispenser-launched munition with two-stage spin-imparting vanes
DE2609932C2 (en) * 1976-03-10 1984-04-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Folding tail for missiles
US4158447A (en) * 1977-11-29 1979-06-19 The United States Of America As Represented By The Secretary Of The Navy Expanding stabilizing fin cup
US4383831A (en) * 1978-09-05 1983-05-17 Raytheon Company Stabilized suspension system
US4336914A (en) * 1978-12-29 1982-06-29 The Commonwealth Of Australia Deployable wing mechanism
DE3516367A1 (en) * 1985-05-07 1986-11-13 Diehl GmbH & Co, 8500 Nürnberg Missile having folding wings
US5040746A (en) * 1990-08-14 1991-08-20 The United States Of America As Represented By The Secretary Of The Army Finned projectile with supplementary fins
US5085381A (en) * 1991-03-29 1992-02-04 The United States Of America As Represented By The Secretary Of The Air Force Deployable aerodynamic aerosurface
US5417393A (en) * 1993-04-27 1995-05-23 Hughes Aircraft Company Rotationally mounted flexible band wing
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
CN110749247A (en) * 2018-07-23 2020-02-04 沈阳航盛科技有限责任公司 External throwing type active bait bomb

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR929040A (en) * 1946-06-14 1947-12-15 Device for folding and deploying the fins of mobile empennés
FR1061242A (en) * 1952-08-05 1954-04-09 Development of rocket projectiles with deployable tail fins
NL93582C (en) * 1953-04-23
GB745252A (en) * 1953-07-29 1956-02-22 Ml Aviation Co Ltd Improvements relating to rocket propelled projectiles
BE533456A (en) * 1953-12-21 Brandt Soc Nouv Ets
NL211396A (en) * 1955-10-20 Brandt Soc Nouv Ets
US2918235A (en) * 1955-12-31 1959-12-22 Aberg Lars Douglas Parachute devices

Also Published As

Publication number Publication date
US3165281A (en) 1965-01-12
DE1159314B (en) 1963-12-12

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